CN203561468U - High-precision torque test component under thermal vacuum environment - Google Patents
High-precision torque test component under thermal vacuum environment Download PDFInfo
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- CN203561468U CN203561468U CN201320584294.8U CN201320584294U CN203561468U CN 203561468 U CN203561468 U CN 203561468U CN 201320584294 U CN201320584294 U CN 201320584294U CN 203561468 U CN203561468 U CN 203561468U
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- air supporting
- supporting cover
- transmission shaft
- measured piece
- output shaft
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Abstract
The utility model discloses a high-precision torque test component under thermal vacuum environment, and relates to the field of sealed test devices in thermal vacuum experiments. The thermal vacuum tank is provided with a thermal vacuum layer and a near normal temperature vacuum layer. Under a high temperature environment, a device is easy to deform, so an angle measurement device is disposed in the near normal temperature vacuum layer to perform high precision measurement on angles. Through a driving lever connecting with a measured piece output shaft and a transmission shaft, influence on transmission of axis offset of a work piece caused by deformation under high temperature is eliminated. The torque of the workpiece is measured on the transmission shaft, and angles are measured by a sine flange plate disposed on the measured piece output shaft. The torque test component comprises magnetic core assemblies which are sleeved on the transmission shaft and play a role of sealing. The transmission shaft is sleeved with two flotation sleeves, forming flotation support on the transmission shaft, preventing the transmission shaft to bend. Since a flotation device is advantaged by no friction, influence of friction forces of a plain bearing on torque measurement is prevented, and test precision is further improved.
Description
Technical field
The utility model relates to the sealing test device under a kind of thermovacuum experiment, relates in particular to the High Precision Torque Measuring parts under a kind of hot vacuum environment.
Background technology
Thermal vacuum test refers to the test of testing performance and the function of measured piece under the vacuum of regulation and thermal cycle conditions.Thermal vacuum test not only needs there is the vacuum-simulating system that can simulate outer space vacuum environment, and need to have and can equipment be driven or be loaded with the suffered driving of simulation mechanism and load device, also to possess the ability of the information such as torque, corner and the rotating speed of real-time high-precision measuring equipment simultaneously.
Measured piece being reversed in the thermal vacuum test loading, under hot vacuum environment, the reliability decrease of sensor, power-equipment, shorten serviceable life, is difficult to control in test process, and therefore often adopting the outer simulation system of thermovacuum is that vacuum tank is tested outward.The outer test of tank refers to the outside that transmits torque to vacuum tank by packoff, and the test of torque is carried out outward at vacuum tank.
Loading as outer in tank and measurement mechanism are fixedly tested by the motor output shaft to be measured in transmission shaft and tank, to analyze each characteristic of motor under hot vacuum environment, if also need to measure the no-load characteristic of motor, in test process, need motor output shaft and transmission shaft to throw off, this difficulty under hot vacuum environment is very large.If measured piece is shaft coupling etc., need the outer loading of two-way shaft and tank and measurement mechanism to be connected.
Thermal vacuum test system often adopts magnetic fluid seal driving device to be connected with measured piece in vacuum tank, rotary magnetic Fluid Sealing axle can meet assurance hot vacuum environment seal request on the one hand, also can realize on the other hand vacuum tank outer to the power transmission in tank, if number of patent application is 200710068382.1, " magnetofluid seal driving device for vacuum equipment driving shaft " discloses and a kind ofly adopts that accuracy of detection is high, the magnetic fluid seal driving device of good reliability.Number of patent application be 201010243123.X's " device for sealing magnetic fluid " a kind of magnetic sealing means is also disclosed; Because sensor measurement mechanism is positioned at outside thermovacuum simulation system, this has become indirect measurement with regard to making to the measurement of measured piece information in thermovacuum simulated environment, magnetic fluid seal driving device self friction power consumption is little, but magnet fluid sealing axle both sides need bearings to guarantee not deflect, if use bearings, the friction force of bearing can produce impact greatly to torque measurement; Measured piece is fixedly linked by the loading outside magnetic fluid seal driving device and tank and measurement mechanism, because measured piece can produce distortion under hot vacuum environment, and measured piece is fixed in tank, distortion can affect being connected of measured piece and magnet fluid sealing axle, make it connect axle center and change, produce the result of the impact tests such as deflection.
Utility model content
For problems such as the frictional influences of measured piece deformation in thermovacuum torsion test and magnetic fluid seal driving device, the utility model provides a kind of High Precision Torque Measuring parts of eliminating under hot vacuum environment friction force, that be not subject to measured piece deformation effect.
The utility model solves the technical scheme that its technical matters adopts: the High Precision Torque Measuring parts under a kind of hot vacuum environment, comprise thermovacuum tank and measured piece, and in described thermovacuum tank, be provided with heat sinkly, measured piece connects measured piece output shaft, it also comprises transmission shaft, air supporting cover, nonmagnetic seat, core assembly, described air supporting cover comprises the first air supporting cover and the second air supporting cover, described core assembly, the first air supporting cover, the second air supporting cover is sleeved on transmission shaft successively, described core assembly and the first air supporting cover, the certain distance in interval between the first air supporting cover and the second air supporting cover, described nonmagnetic cover for seat is contained in the first air supporting cover, the second air supporting cover, on core assembly, described transmission shaft and the first air supporting cover, between the second air supporting cover, there is minim gap, described nonmagnetic seat is provided with two radial air inlet holes, described radial air inlet hole communicates with the inlet chamber that two air supportings put respectively, described nonmagnetic seat left end and thermovacuum tank are fixed, described nonmagnetic seat right-hand member is installed end cap, described nonmagnetic seat is positioned at the gap portion of core assembly and the first air supporting cover and the radially uniform bleeder port of gap portion of the first air supporting cover and the second air supporting cover, described transmission shaft is through thermovacuum tank, the left end of described transmission shaft is connected by deflector rod device with measured piece input shaft, measured piece output shaft is through heat sink, the outer loading equipemtn of the external thermovacuum tank of described transmission shaft right-hand member and torque sensor,
One end of described measured piece output shaft is through heat sink connection measured piece, measured piece output shaft is positioned in the part on heat sink right side and is set with sinusoidal ring flange, laser acquisition head is housed on thermovacuum tank, laser acquisition head can read the distance between laser acquisition head and sinusoidal ring flange, by output line output signal;
Described deflector rod device comprises driving lever, spring, pulley, square boss, described square boss is fixed on the end face of rotation axis, and described driving lever is provided with four, one end of driving lever connects measured piece output shaft, four driving levers distribute symmetrically at survey part output shaft end face, and the other end of four driving levers all connects four pulleys by spring, and four pulleys lean against the two sides of square boss;
Described core assembly comprises two annular magnetic poles, permanent magnet, and described permanent magnet is between two annular magnetic poles, and the inside surface of described annular magnetic pole is provided with utmost point mark of mouth groove, between the minim gap of described utmost point mark of mouth groove and transmission shaft, is provided with sealing magnetic fluid; Described nonmagnetic seat is provided with the filling hole of magnetic fluid;
Between described nonmagnetic seat and thermovacuum tank, be provided with a 〇 RunddichtringO, between described two annular magnetic poles and nonmagnetic seat, be provided with and establish the 2nd 〇 RunddichtringO, between described first, second air supporting cover outer ring and nonmagnetic seat, the 3rd 〇 RunddichtringO is installed.
Mentality of designing of the present utility model and advantage show: on transmission shaft, be set with core assembly and play sealing function, on transmission shaft, be set with two air supporting covers, by the radial air inlet hole air feed on nonmagnetic seat, can on transmission shaft, form stable air film, two certain distances in air supporting cover interval, form air supporting to transmission shaft and support, prevent that transmission shaft from occurring bending, due to air-floating apparatus friction free advantage, avoided the friction force of plain bearing on the impact of torque measurement, further improved measuring accuracy.
What in thermovacuum tank, be provided with is heat sinkly divided into thermovacuum layer and near ambient temperature vacuum layer by thermovacuum tank, at hot environment lower device, easily produce distortion, therefore we are installed in angle measurement unit near ambient temperature vacuum layer and carry out the high-acruracy survey of angle, simultaneously, by driving lever, connect measured piece output shaft and transmission shaft, eliminate workpiece and be at high temperature out of shape the desaxe of generation to the impact of transmission, the moment of torsion of measuring workpieces on transmission shaft, utilizes the sinusoidal ring flange of installing on measured piece output shaft to take measurement of an angle.
Laser acquisition head is measured laser acquisition head and sinusoidal ring flange apart from S, when ring flange is from 0 angle rotation φ angle, S=± Asin(φ), distance becomes sine relation with angle, therefore with the distance S between laser acquisition head and sinusoidal ring flange, can calculate the angle φ of shaft rotation.
Accompanying drawing explanation
Fig. 1 is the structural representation of the High Precision Torque Measuring device under hot vacuum environment.
Fig. 2 is A-A cross section partial enlarged drawing.
Fig. 3 is the stretch-out view of sinusoidal ring flange.
Embodiment
Now by reference to the accompanying drawings the utility model is further detailed.
By reference to the accompanying drawings 1, accompanying drawing 2, High Precision Torque Measuring parts under a kind of hot vacuum environment, comprise thermovacuum tank 2 and measured piece 6, in thermovacuum tank 2, be provided with heat sink 8, measured piece 6 connects measured piece output shaft 5, this device also comprises transmission shaft 1, air supporting cover, nonmagnetic seat 14, core assembly, air supporting cover comprises the first air supporting cover 3 and the second air supporting cover 4, core assembly, the first air supporting cover 3, the second air supporting cover 4 is sleeved on transmission shaft 1 successively, core assembly and the first air supporting cover 3, the certain distance in interval between the first air supporting cover 3 and the second air supporting cover 4, nonmagnetic seat 14 is sleeved on the first air supporting cover 3, the second air supporting cover 4, on core assembly, transmission shaft 1 and the first air supporting cover 3, between the second air supporting cover 4, there is minim gap, nonmagnetic seat is provided with two radial air inlet holes 13, radial air inlet hole 13 communicates with the inlet chamber that two air supportings put respectively, nonmagnetic seat 14 left ends and thermovacuum tank 2 are fixing, nonmagnetic seat 14 right-hand members are installed end cap 17, nonmagnetic seat 14 is positioned at the gap portion of core assembly and the first air supporting cover 3 and the radially uniform bleeder port 12 of gap portion of the first air supporting cover 3 and the second air supporting cover 4, transmission shaft 1 is through thermovacuum tank 2, the left end of transmission shaft 1 is connected by deflector rod device with measured piece input shaft 5, measured piece output shaft 5 is through heat sink 8, the outer loading equipemtn of the external thermovacuum tank of transmission shaft 1 right-hand member and torque sensor.
Measured piece 6 is fixing with thermovacuum tank 2 by base 7.
One end of measured piece output shaft 5 connects measured piece 6 through heat sink 8, measured piece output shaft 5 is positioned in the part on heat sink 8 right sides and is set with sinusoidal ring flange 9, laser acquisition 16 is housed on thermovacuum tank, laser acquisition 16 can read on laser acquisition 16 and sinusoidal ring flange 9 between distance, thereby calculate the angle of shaft rotation.
Deflector rod device comprises driving lever 19, spring 20, pulley 21, square boss 18, square boss 18 is fixed on the end face of transmission shaft 1, and driving lever 19 is provided with four, one end of driving lever 19 connects measured piece output shaft 5, four driving levers 19 distribute symmetrically at measured piece output shaft 5 end faces, and the other end of four driving levers 19 is all connected 21, four pulleys 21 of four pulleys and leaned against the two sides of square boss 18 by spring 20.By deflector rod device, connect measured piece output shaft 5 and transmission shaft 1, eliminating workpiece deformation is that desaxe brings the impact on measuring.
Core assembly comprises two annular magnetic poles 10, permanent magnet 11, and permanent magnet 11 is between two annular magnetic poles 10, and the inside surface of annular magnetic pole 10 is provided with utmost point mark of mouth groove 15, between the minim gap of utmost point mark of mouth groove 15 and transmission shaft 1, is provided with sealing magnetic fluid; Nonmagnetic seat 14 is provided with the filling hole of magnetic fluid.
Between nonmagnetic seat 14 and thermovacuum tank 2, there is a 〇 RunddichtringO, between two annular magnetic poles 10 and nonmagnetic seat 14, the 2nd 〇 RunddichtringO is installed, between two air supporting cover outer rings and nonmagnetic seat 14, the 3rd 〇 RunddichtringO is installed.
Claims (1)
1. the High Precision Torque Measuring parts under hot vacuum environment, comprise thermovacuum tank and measured piece, are provided with heat sinkly in described thermovacuum tank, and measured piece connects measured piece output shaft, it is characterized in that: it also comprises transmission shaft, air supporting cover, nonmagnetic seat, core assembly, described air supporting cover comprises the first air supporting cover and the second air supporting cover, described core assembly, the first air supporting cover, the second air supporting cover is sleeved on transmission shaft successively, described core assembly and the first air supporting cover, the certain distance in interval between the first air supporting cover and the second air supporting cover, described nonmagnetic cover for seat is contained in the first air supporting cover, the second air supporting cover, on core assembly, described transmission shaft and the first air supporting cover, between the second air supporting cover, there is minim gap, described nonmagnetic seat is provided with two radial air inlet holes, described radial air inlet hole communicates with the inlet chamber that two air supportings put respectively, described nonmagnetic seat left end and thermovacuum tank are fixed, described nonmagnetic seat right-hand member is installed end cap, described nonmagnetic seat is positioned at the gap portion of core assembly and the first air supporting cover and the radially uniform bleeder port of gap portion of the first air supporting cover and the second air supporting cover, described transmission shaft is through thermovacuum tank, the left end of described transmission shaft is connected by deflector rod device with measured piece input shaft, measured piece output shaft is through heat sink, the outer loading equipemtn of the external thermovacuum tank of described transmission shaft right-hand member and torque sensor,
One end of described measured piece output shaft is through heat sink connection measured piece, measured piece output shaft is positioned in the part on heat sink right side and is set with sinusoidal ring flange, laser acquisition head is housed on thermovacuum tank, laser acquisition head can read laser acquisition head and sinusoidal ring flange distance, by output line output signal;
Described deflector rod device comprises driving lever, spring, pulley, square boss, described square boss is fixed on the end face of rotation axis, and described driving lever is provided with four, one end of driving lever connects measured piece output shaft, four driving levers distribute symmetrically at survey part output shaft end face, and the other end of four driving levers all connects four pulleys by spring, and four pulleys lean against the two sides of square boss;
Described core assembly comprises two annular magnetic poles, permanent magnet, and described permanent magnet is between two annular magnetic poles, and the inside surface of described annular magnetic pole is provided with utmost point mark of mouth groove, between the minim gap of described utmost point mark of mouth groove and transmission shaft, is provided with sealing magnetic fluid; Described nonmagnetic seat is provided with the filling hole of magnetic fluid;
Between described nonmagnetic seat and thermovacuum tank, be provided with a 〇 RunddichtringO, between described two annular magnetic poles and nonmagnetic seat, be provided with and establish the 2nd 〇 RunddichtringO, between described first, second air supporting cover outer ring and nonmagnetic seat, the 3rd 〇 RunddichtringO is installed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320584294.8U CN203561468U (en) | 2013-09-18 | 2013-09-18 | High-precision torque test component under thermal vacuum environment |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320584294.8U CN203561468U (en) | 2013-09-18 | 2013-09-18 | High-precision torque test component under thermal vacuum environment |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203561468U true CN203561468U (en) | 2014-04-23 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320584294.8U Withdrawn - After Issue CN203561468U (en) | 2013-09-18 | 2013-09-18 | High-precision torque test component under thermal vacuum environment |
Country Status (1)
| Country | Link |
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| CN (1) | CN203561468U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103512691A (en) * | 2013-09-18 | 2014-01-15 | 浙江工业大学 | High-accuracy torque testing component in thermal vacuum environment |
| CN113776824A (en) * | 2021-09-15 | 2021-12-10 | 北京卫星环境工程研究所 | High-precision dynamic micro friction torque testing system applied to space environment test |
-
2013
- 2013-09-18 CN CN201320584294.8U patent/CN203561468U/en not_active Withdrawn - After Issue
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103512691A (en) * | 2013-09-18 | 2014-01-15 | 浙江工业大学 | High-accuracy torque testing component in thermal vacuum environment |
| CN103512691B (en) * | 2013-09-18 | 2015-05-27 | 浙江工业大学 | High-accuracy torque testing component in thermal vacuum environment |
| CN113776824A (en) * | 2021-09-15 | 2021-12-10 | 北京卫星环境工程研究所 | High-precision dynamic micro friction torque testing system applied to space environment test |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20140423 Effective date of abandoning: 20150527 |
|
| AV01 | Patent right actively abandoned |
Granted publication date: 20140423 Effective date of abandoning: 20150527 |
|
| RGAV | Abandon patent right to avoid regrant |